Airbus A300-600 vs. North American B-25 Mitchell
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Airbus A300-600 |
versus |
North American B-25 Mitchell |
54.10 m |
177 ft 6 in |
length |
16.15 m |
53 ft 0 in |
16.5 m |
54 ft 2 in |
height |
5 m |
16 ft 4 in |
44.84 m |
147 ft 1 in |
wingspan |
20.58 m |
67 ft 6 in |
2 x turbofan engines, either Pratt & Whitney PW 4000 or General Electric GE CF6-80C2A1 |
engines |
2 x Wright R-2600-92 Twin Cyclone |
56,000lb to 61,500lb |
thrust per engine |
1,700 horsepower |
112,000–123,000 lb |
total thrust |
3,400 horsepower |
171,700 kg |
378,600 lb |
MTOW |
7,484 kg |
16,500 lb |
7,500 km |
4,052 nm |
range |
1,350 mi |
1,175 nm |
897 km/h |
557 mph |
cruise speed |
233 MPH |
375 km/h |
210-250 passengers |
capacity |
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rotor diameter |
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rate of climb |
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Please note that these values are indicative and actual values can vary based on specific engine models and configurations.